The trajectory of the Object was observed to be changed from every detonation in addition to revealing the strength of the detonation and the angle of the detonation impact.

Thus any projected Orbital coordinate based projection would be impractical in this unfolding sequence. Only a trigonometric solution method was used to keep up with these events.

Recent history of Coordinate changes:

The object originally had an EE Latitude vector of 27.5 degrees North. The first two detonations changed the EE Latitude & velocity such that it changed from 27.5 N to 21.0 N.

The next two to three detonations changed it from 21.0N to 16.0N with an average of 2 degrees per day change from 16.0 N. A large detonation was a “direct hit” angle which slowed the object significantly, but the 2 degrees per day remained.

The final large detonation caused a single day angle shift near 4 degrees in Latitude (6.25 to 2.5 degrees EE Latitude North).

This final large detonation boosted the velocity of the object besides the notable angle shift.

This last intervention put the object into an escape from Earth’s Gravity Well, but just enough (determined by an Earth Escape Velocity at a LD distance).

Earth literally moving away from Object:

The object to Earth distance differential is increasing at just over the velocity of the Earth orbit km/s around the sun + the low speed of the slowed and redirected “Object”.

This is mainly due to the object reduced to nearly a virtual standstill compared to typical Asteroid velocities.

This means that any Astronomers looking for this object should be aware of this slow movement rate (0.163 km/s) when using differential detection process using the backdrop of stars.